N647DL

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 76,571 hrs · 33,393 cycles

C/W ER/A 06-496073-14 REV A. RII INSPECTION INSTRUCTIONS. ATLMA MWG 11SEP C/W ERA 06-496073-14 REV A RII INSPECTION SECTION I. TEMPORARY REPAIR. PER ERA 06-496024-14MA REV A.

Part: CIRCUIT BREAKER — FAILED (LT GENERATOR) · airframe 73,840 hrs · 32,414 cycles

THE AUTOPILOT AUTOMATICALLY DISCONNECTED AND THE LT GENERATOR TRIPPED OFF ACCOMPANIED BY A LT BUSS EICAS MESSAGES. FLIGHT CREW ATTEMPTED TO RESET THE GENERATOR SEVERAL TIMES UNTIL EVENTUALLY ELECTRICAL FUMES WERE NOTED. AN EMERGENCY WAS DECLARED AND THE FLIGHT DIVERTED TO A NORMAL SAFE LANDING. MX REPLACED THE LT GENERATOR BREAKER, THE LT BTB, AND THE GCU. ALL SYS CHECKS AND RUN-UP WERE GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 72,796 hrs · 32,064 cycles

DURING AN A-CHECK, MAINTENANCE FOUND THE EXTERIOR EMERGENCY LIGHT AFT OF DOOR 3L INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY. OPERATIONAL CHECK WAS GOOD (ODI 2010-D0934)(DL757102000).

Part: WEB — CORRODED (FUSELAGE) · airframe 65,438 hrs · 29,657 cycles

RT SIDE MAIN CABIN FLOOR STRUCTURE IS CORRODED AT FS 1420-1440 LOWER WEB FWD END. REPLACED DAMAGED WEB IAW SRM'S 51-20-02 AND 51-40-02.

Part: SLIDE — FAILED (LT OFF WING) · airframe 65,438 hrs · 29,657 cycles

LT OFF WING ESCAPE FAILED PNEUMATIC DEPLOYMENT OPS CHECK. REPLACED LT OFF WING ESCAPE SLIDE ACTUATOR IAW AMM 25-65-05. LEAK AND OPS CHECK GOOD.

Part: STRUCTURE — DENTED (COCKPIT) · airframe 65,438 hrs · 29,657 cycles

COCKPIT FLOOR HAS DEEP DENT AT ENTRY. DOUBLER REPAIRED DAMAGE IAW SRM 51-20-01.

Part: FRAME — DENTED (FUSELAGE) · airframe 65,438 hrs · 29,657 cycles

AFT CARGO PIT STA 1540 LT FRAME AT STR 23L HAS A DENT. REPLACED DAMAGED FRAME FLANGE IAW SRM 53-00-07.

Part: SKIN — DENTED (AFT CARGO DOOR) · airframe 65,421 hrs · 29,651 cycles

RAMP REPORTS 2 MINOR DENTS IN AFT CARGO DOOR. 1ST APPROX 8 IN BELOW HANDLE AFT EDGE. 2ND APPROX 7 IN AFT AND 4 IN UP FROM FWD CORNER OF DOOR. DENT AT FWD CORNER OF DOOR FOUND TO BE OUT OF LIMITS. REPLACED REPAIR DOUBLER IAW SRM 51-40-01.

Part: ANGLE — CORRODED (BS 1540-1560) · airframe 65,405 hrs · 29,644 cycles

AFT CARGO PIT STA 1540-1560 STR 27R WEB "L" ANGLE CORRODED. REPLACED "L" ANGLE IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 65,405 hrs · 29,644 cycles

MAIN CABIN STA 365 SEAT TRACK AT RBL 45 HAS SEVERE CORROSION, EXFOLIATED. REPLACED DAMAGED SEAT TRACK IAW SRM'S 51-40-02 AND 53-10-52.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 65,405 hrs · 29,644 cycles

CABIN L4 DOOR CUTOUT, FWD FRAME AT FLOOR LEVEL 5 IN FWD OF DOOR FRAME CORRODED. REPAIRED DAMAGED SECTION IAW SRM'S 53-60-15, 51-10-02 AND ERA 468357-14.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 65,405 hrs · 29,644 cycles

MAIN CABIN FLOOR STRUCTURE DECK PLATE REPAIR DOUBLER HAS CORROSION STA 1715 LBL 12. REPLACED DOUBLER IAW SRM 51-40-02.

Part: FRAME — DENTED (FUSELAGE) · airframe 65,405 hrs · 29,644 cycles

AFT CARGO PIT STA 1540 LT FRAME AT STR 23L HAS A DENT. REPAIRED DENT IAW SRM 53-00-07.

Part: FLOOR SUPPORT — CORRODED (FS 377.7) · airframe 65,405 hrs · 29,644 cycles

MAIN CABIN FS 377.7 LBL 3-10 HAS CORROSION WHERE FLOOR PANEL SITS. REPLACED ANGLE IAW SRM 53-10-51.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 65,405 hrs · 29,644 cycles

UPON REMOVAL OF DOME NUT PLATE, FOUND EXFOLIATION CORROSION IN CHANNEL OF S 20R STA 758. REPLACED DAMAGED SECTION OF STRINGER IAW SRM 53-30-03 FIG 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 65,405 hrs · 29,644 cycles

MAIN CABIN SEAT TRACK STARTING AT FS 630 LBL 45 TO FS 790 HAS NUMEROUS AREAS OF CORROSION DAMAGE. REPAIRED SEAT TRACK IAW SRM 53-30-52.

Part: SKIN — DENTED (FUSELAGE) · airframe 65,405 hrs · 29,644 cycles

DENT ON LT SIDE FUSELAGE STA 408 GOES ACROSS STR 16L AND 2 BAYS. REPAIRED DAMAGE IAW SRM 53-00-01.

Part: SKIN — CHAFED (NR 3 SLAT) · airframe 65,405 hrs · 29,644 cycles

LT WING NR 3 SLAT AT T/E AREA HAS CHAFING 2 EA LOCATIONS. REPAIRED CHAF IAW SRM 51-70-10.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 65,405 hrs · 29,644 cycles

AFT CARGO PIT STA 1360-1380 WEB "L" ANGLE BETWEEN S 27R AND 26R CORRODED. REPLACED "L" ANGLE IAW SRM 51-10-01 AND 53-60-04.

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 65,405 hrs · 29,644 cycles

MAIN CABIN STA 1640 LBL FLOOR STRUCTURE "T" CHORD REPAIR EXFOLIATED AT FASTENER HOLE. REPLACED DAMAGED FLOOR STRUCTURE IAW SRM 53-00-51.

Part: WEB — CORRODED (FUSELAGE) · airframe 65,405 hrs · 29,644 cycles

RT SIDE MAIN CABIN FLOOR STRUCTURE IS CORRODED AT FS 1420-1440 LOWER WEB FWD END. REPLACED DAMAGED WEB IAW SRM 51-40-02.

Part: GROUND WIRE — LOOSE (EVAC SLIDE) · airframe 65,396 hrs · 29,639 cycles

SQUIB AND SWITCH TEST P61 PANEL FAILS TEST 1. TROUBLESHOT L EMERGENCY ESCAPE SLIDE SQUIB AND NR 1 TEST SWITCH ON P61 PANEL IAW WDM 25-65-01. FOUND LOOSE GROUNDS ON CONNECTOR D5544. RECONNECTED LOOSE GROUND WIRES ON CONNECTOR D5544 IAW SWPM 20-20-00. PERFORMED OPS CHECK OF LEFT EMERGENCY ESCAPE SLIDE SQUIB TEST IAW AMM 25-65-00. OPS CHECK GOOD.

Part: VIDEO DISPLAY — BURNED (COCKPIT) · airframe 47,402 hrs · 23,303 cycles

F/A REPORTED SMELL IN CABIN AND ORANGE GLOW COMING FROM VIDEO CONTROLLER UNIT. FOUND VIDEO ON LIGHT ARCED AND SHORTED. REPLACED VIDEO ON LIGHT.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 46,195 hrs · 22,727 cycles

SMOKE REPORTED IN AFT CABIN AT GATE DURING PREFLIGHT. R&R OUTFLOW VALVE ASSY PER M/M. OP CK GOOD.

Part: BOTTLE — LOW (L4 DOOR) · airframe 46,169 hrs · 22,711 cycles

ON L/O FOUND L4 DOOR OPEN ASSIST BOTTLE LOW. REPLACED BOTTLE PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 44,377 hrs · 21,795 cycles

FOUND ON WALKAROUND CHECK, R-1 DOOR; L-1 DOOR ; L-2 DOOR AND LEFT AFT OVERWING EXTERIOR EMERGENCY LIGHTS INOP. RELAMPED, ALL LIGHTS NOW OPERATIONAL CHECK NORMAL.

Part: UPLOCK SENSOR — FAILED (LT MLG) · airframe 44,127 hrs · 21,679 cycles

AFTER T/O, DOOR DISAGREE LIGHT, COCKPIT NOISE AND BUFFET FELT. REPLACED UP LOCK SENSOR.

Part: HYDRAULIC LINE — LEAKING (HYD SYSTEM) · airframe 42,336 hrs · 20,804 cycles

AFTER TAKEOFF GEAR DOORS LIGHT AND ADVISORY MESSAGE ON WHEN GEAR RAISED. GEAR RECYCLED, LIGHT STILL ON. FLT ATTN REPORTS VIBRATION IN FLOOR NEAR GEAR DOOR AREA. FOUND FLEX HYD LINE LEAKING ABOVE RT MLG. MADE APPROVED HYD REPAIR. INSTALLED TEMP HYD LINE PER MM 20-10-09, TIME LIMITED 350 HRS. LEAK CKS GOOD. P/N 326201061 HOSE P/N 00AE90-6D052 FWD TO MCO/PLAC.

Part: WARNING — ACTIVATED (SPOILER SYS)

FIRST FLIGHT OF THE DAY DELAY AIRCRAFT 647, ABORTED T/O TWICE FOR SPOILER WARNING. AFTER FIRST T/O ABORT, SPOILERS WERE VISUALLY CHECKED AND RELATED COMPONENTS CHECKED, SHOWED NO FAULTS. LOG ENTRY MADE, AIRCRAFT DEPARTED GATE. ON SECOND T/O ABORT, SPOILER WARNING AND T/O CONFIG CAME ON. AIRCRAFT RETURNED TO GATE. FOUND T/O CONFIG WARNING CARD M620 BAD. REPLACED CARD, ALL SYSTEMS CHECKED NORMAL. AIRCRAFT DEPARTED PDX OK. FIRST ABORT SPEED 80 KNOTS, SECOND ABORT SPEED 40 KNOTS. NO DANGER REPORTED BY CREW DURING BOTH T/O ATTEMPTS. NO DANGER TO PASSENGERS OR CREW.

Part: ACTUATOR — CRACKED (NR 1 ENG)

DURING CLIMB-OUT, LEFT ENG WOULD NOT REACH COMMANDED CLIMB EPR N2 IND 100 FF MATCHED RT ENG EVENT RECORD PUSHED AT HIGHER ALT. LEFT ENG EPR IND CONT TO FALL OFF OIL TEMP REACHED 129. REPLACED STATOR VANE ACTUATOR AND BRACKET.

Part: COMPRESSOR FAN — BIRD STRIKE (NR 2 ENGINE)

RT ENG FAILED AT APPROX 800 FT DUE TO INGESTION OF LARGE BIRD. REQUIRES ENG CHANGE, HEAVY FAN AND NOSE COWL DAMAGE.

Part: PANEL — HEAT DAMAGE (ENGINE)

DURING SHOP VISIT AT REPAIR STATION EZ2R812K, ENGINE FAN COWL WAS REPAIRED FOR HEAT DAMAGE ON INTERIOR SKIN AT LOWER FWD END. A 2 SQ FT AREA OF HONEY COMB WAS REMOVED AND REPLACED PER DRAWING 314N3111, SRM 54-21-01 AND 54-21-04.